Experimental validation of FEM-computed stress to tip deflection ratios of aero-engine compressor blade vibration modes and quantification of associated uncertainties

Number of the records: 1

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SYSNO	0563591
Title	Experimental validation of FEM-computed stress to tip deflection ratios of aero-engine compressor blade vibration modes and quantification of associated uncertainties
Author(s)	Mohamed, E.M. (GB) Bonello, P. (GB) Russhard, P. (GB) Procházka, Pavel (UT-L)_{RID, ORCID} Mekhalfia, Mohammed Lamine (UT-L) Tchawou Tchuisseu, Eder Batista (UT-L)_ORCID
Source Title	Mechanical Systems and Signal Processing. Roč. 178, October (2022). - : Elsevier
Article number	109257
Document Type	Článek v odborném periodiku
Grant	EF15_003/0000493 GA MŠMT - Ministry of Education, Youth and Sports (MEYS), CZ - Czech Republic
	StrategieAV21/3, CZ - Czech Republic
Institutional support	UT-L - RVO:61388998
Language	eng
Country	GB
Keywords	blade tip timing * FEM validation * vibration measurements * blade stresses
Cooperating institutions	University of Manchester (United Kingdom) EMTD Ltd. (United Kingdom)
URL	https://www.sciencedirect.com/science/article/pii/S0888327022004058/pdfft?isDTMRedir=true&download=true
Permanent Link	https://hdl.handle.net/11104/0335685

Number of the records: 1